The invention relates to an elongated antenna assembly (1) for an aircraft. The antenna assembly (1) comprises a structural portion (3) and an antenna element (5), wherein the structural portion (3) comprises an elongate leading edge portion (7) extending in a longitudinal direction (13) of the antenna assembly, a first lateral portion (9) and a second lateral portion (11), the leading edge portion (7) is curved and comprises a convex outer surface (15) extending on a convex side (19) of the antenna assembly in a longitudinal direction (13) of the antenna assembly, and the first lateral portion (9) extends away from the leading edge portion (7) on a second side (23) of the leading edge portion (7) in a second direction (39) transverse to the longitudinal direction (13) of the antenna assembly. The second lateral portion (11) extends away from the leading edge portion (7) on a second side (25) of the leading edge portion (7) opposite the first side (23) of the leading edge portion (7) in a second direction (41) transverse to the longitudinal direction (13) of the antenna assembly, and an elongated first recess is formed in the leading edge portion (7) on a convex side (19) of the antenna assembly, the first recess extends in a longitudinal direction (13) of the antenna assembly, and an elongated first portion (27) of the antenna element (5) extends in the longitudinal direction (13) of the antenna assembly (1) and is arranged in the first recess, the outer surface (43) of the elongated first portion (27) of the antenna element (5) and the convex outer surface (15) of the leading edge portion (7) form the first surface of the antenna assembly (1) on the convex side (19) of the antenna assembly.

    本发明涉及一种用于飞行器的长形的天线组件(1)。天线组件(1)包括结构部分(3)和天线元件(5),其中,结构部分(3)包括沿天线组件的纵向方向(13)延伸的长形前缘部分(7)、第一侧向部分(9)和第二侧向部分(11),其中,前缘部分(7)是弯曲的,使得前缘部分(7)包括在天线组件的凸形侧部(19)上沿天线组件(1)的纵向方向(13)延伸的凸形外表面(15),其中,第一侧向部分(9)在前缘部分(7)的第一侧部(23)上沿横向于天线组件的纵向方向(13)的第一方向(39)远离前缘部分(7)延伸,其中,第二侧向部分(11)在前缘部分(7)的与前缘部分(7)的第一侧部(23)相反的第二侧部(25)上沿横向于天线组件的纵向方向(13)的第二方向(41)远离前缘部分(7)延伸,其中,在天线组件的凸形侧部(19)上于前缘部分(7)中形成有长形的第一凹部,其中,第一凹部沿天线组件的纵向方向(13)延伸,其中,天线元件(5)的长形的第一部分(27)沿天线组件(1)的纵向方向(13)延伸并且布置在第一凹部中,使得天线元件(5)的长形的第一部分(27)的外表面(43)和前缘部分(7)的凸形外表面(15)在天线组件的凸形侧部(19)上形成天线组件(1)的第一表面。


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    Title :

    Antenna assembly, vertical tail, horizontal tail, wing, aircraft and method


    Additional title:

    天线组件、竖向尾翼、水平尾翼、机翼、飞行器和方法


    Contributors:

    Publication date :

    2021-09-10


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge / H01Q Antennen , ANTENNAS, i.e. RADIO AERIALS



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